GB131648A - - Google Patents

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Publication number
GB131648A
GB131648A GB131648DA GB131648A GB 131648 A GB131648 A GB 131648A GB 131648D A GB131648D A GB 131648DA GB 131648 A GB131648 A GB 131648A
Authority
GB
United Kingdom
Prior art keywords
blades
resultant
pressure
levasseur
deflexion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
Other languages
English (en)
Publication of GB131648A publication Critical patent/GB131648A/en
Active legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB131648D Active GB131648A (enExample)

Publications (1)

Publication Number Publication Date
GB131648A true GB131648A (enExample)

Family

ID=1725198

Family Applications (1)

Application Number Title Priority Date Filing Date
GB131648D Active GB131648A (enExample)

Country Status (1)

Country Link
GB (1) GB131648A (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451106A (en) * 1944-04-22 1948-10-12 United Aircraft Corp Propeller blade construction
US3851994A (en) * 1972-01-20 1974-12-03 Bbc Brown Boveri & Cie Blading for axial flow turbo-machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451106A (en) * 1944-04-22 1948-10-12 United Aircraft Corp Propeller blade construction
US3851994A (en) * 1972-01-20 1974-12-03 Bbc Brown Boveri & Cie Blading for axial flow turbo-machine

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